Gain balanced nonlinear optical interferometer

ABSTRACT

A nonlinear fiber interferometer is disclosed suitable for fiber sensor and other applications. A first nonlinear fiber section amplifies probe and conjugate sidebands of a pump through four-wave mixing. A second section introduces a phase shift to be measured, for example from a sensor. A third nonlinear fiber section amplifies with phase-sensitive gain to increase signal-to-noise ratio. Based on phase-sensitive output power of probe and/or conjugate components, the phase shift can be measured. Superior performance can be obtained by balancing gain between the (first and third) nonlinear sections. Non-fiber, for example photonic integrated circuit, embodiments are disclosed. Differential sensing, alternative detection schemes, sensing applications, associated methods, and other variations are disclosed.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application claims the benefit of U.S. Provisional Application No.62/669,470, filed on May 10, 2018, the content of which is incorporatedherein by reference in its entirety.

ACKNOWLEDGMENT OF GOVERNMENT SUPPORT

This invention was made with government support under Contract No.DE-AC05-00OR22725 awarded by the U.S. Department of Energy. Thegovernment has certain rights in the invention.

BACKGROUND

A wide range of optical sensing applications are known. Commonly, amedium in an optical device has a property (e.g., refractive index)which is sensitive to an external parameter (e.g., temperature). Lightpropagating in the medium can experience a change in a detectableproperty (e.g., phase) which can be measured outside the optical device,sometimes at a considerable distance, to infer a value of the sensedparameter.

Some applications can be limited by performance, e.g. a sensed parametercannot be measured with a desired resolution because of noise. Someapplications can be limited by complexity, for example, a requirementfor a high-power laser with its attendant power and cooling systems, orassorted auxiliary devices to compensate for various confounding effectsboth within an optical sensing apparatus (e.g., scattering) or due toexternal influences (e.g., mechanical vibration).

Accordingly, there remains ample opportunity for improvements in opticalsensing.

SUMMARY

Apparatus and methods are disclosed for optical devices, such asinterferometers, having two gain-balanced nonlinear stages, each in afiber or other nonlinear lightguide. Between the two nonlinear stages, aphase shift can be applied on a given light component. The phase shiftcan be detected following phase-sensitive gain in the second nonlinearstage. The phase-sensitive gain can be due to a determinate phaserelationship between several light components as developed in the firstnonlinear lightguide, and a variation in that phase relationship by theapplied phase shift. The applied phase shift can represent a sensedquantity, such as from an optical sensor, and the disclosed technologycan be used for optical sensing in diverse applications.

According to one aspect, the disclosed technologies can be implementedas an optical device incorporating a first nonlinear lightguide, amodulator, and a second nonlinear lightguide. The first nonlinearlightguide has a first length, and is situated to receive seed probelight and pump light from respective lamps. The first nonlinearlightguide is configured to form first mixed light having probe, pump,and conjugate light components. The probe light has a probe gain in thefirst nonlinear lightguide.

The modulator is situated to receive at least a given component of thefirst mixed light from the first nonlinear lightguide and to provide thegiven component to a second nonlinear waveguide, with incorporation of aphase shift representative of a sensed quantity.

The second nonlinear lightguide has a second length, and is situated toreceive second mixed light comprising second probe, second pump, andsecond conjugate components, including the phase-shifted givencomponent. The second nonlinear lightguide is configured to amplify thesecond probe and second conjugate components with phase-sensitive gain.The first length or the second length of the respective nonlinearlightguides is chosen so that averaged phase-sensitive gain matches theprobe gain in the first nonlinear lightguide.

In some examples, a disclosed optical device can also include aphotodetector coupled to an output of the second nonlinear lightguideand configured to measure the second probe component or the secondconjugate component to determine a phase. Further examples can include acontrolled phase shifter coupled to the photodetector, and situated in apath of one of the components of the first mixed light, between thefirst and second nonlinear lightguides.

In additional examples, the optical device can be included in an opticalsensing system, together with a first laser providing the seed probelight is received, and a second laser providing the pump light. Anintrinsic fiber sensor can be sensitive to a parameter and can providephase shift responsive to variations in the parameter. The intrinsicfiber sensor can be coupled to the modulator of such a system. Installedon-board an aircraft, such a system and coupled sensor can monitor aparameter of the aircraft, as an airborne monitoring system. Similarly,such a system and coupled sensor can monitor an environmental parameterof a petrochemical access shaft, as a down-hole environmental monitoringsystem.

In further examples, an output of the photodetector can be coupled to acircuit configured to transform the measured phase into a representationof the sensed quantity, and the disclosed technology can be an opticalsensor. In varying examples, the sensed quantity can be one or more of:temperature, strain, pressure, or angular velocity; and the phase shiftcan be incorporated into the given component by an intrinsic fibersensor that is sensitive to the sensed quantity. Particularly, thesensed quantity can be a pressure wave and the optical sensor can be ahydrophone; or the sensed quantity can be an angular velocity and theoptical sensor can be a gyroscope.

In some examples, at least one of the first or second nonlinearlightguides can be an optical fiber, or at least one of the first orsecond nonlinear lightguides can be a waveguide in a planar lightwavecircuit. The first and second nonlinear lightguides can have matchingcross-sectional structure and matching composition. In some examples,the probe gain can be obtained by pump-degenerate four-wave mixing.

In additional examples, the modulator can incorporate a splitter,configured to separate the given component from other components of thefirst mixed light, and a recombiner configured to merge the givencomponent, with the phase shift incorporated, with other components ofthe second mixed light. The splitter and recombiner can be implementedas an optical add-drop multiplexer (OADM). In certain examples, themodulator can include a first port, for coupling the given componentfrom the splitter to an external fiber sensor, and a second port forcoupling the given component, with the phase shift incorporated, fromthe external fiber sensor to the recombiner. Other examples can includea fiber sensor situated to transport the given component from thesplitter to the recombiner and develop the phase shift in the givencomponent.

In further examples, the seed probe light can be multiplexed between aplurality of wavelengths, the given component of the first mixed lightcan be correspondingly multiplexed between respective sensors for theplurality of wavelengths, and thereby the sensed quantity can bemultiplexed between a respective plurality of quantities detected by therespective sensors.

In a second aspect, the disclosed technologies can be implemented as amethod. Seed probe light is amplified by a first gain in a firstnonlinear lightguide to form first mixed light having first probe, firstpump, and first conjugate components. Second mixed light having secondprobe, second pump, and second conjugate components is provided to asecond nonlinear lightguide. The components of the second mixed lighthave phase relationships with respective components of the first mixedlight. One of the phase relationships is a phase shift associated with asensed quantity. In the second nonlinear lightguide, the second probeand second conjugate components are amplified with phase-sensitive gain.A length of the first or second nonlinear lightguide is selected tomatch an average of the phase-sensitive gain with the first gain.

In some examples, a disclosed method can include splitting a givencomponent from other components of the first mixed light, andrecombining the given component with the other components, with therecombined given component having incorporated a phase shift associatedwith the sensed quantity. In additional examples, an intrinsic fibersensor can receive the split given component, can apply the phase shiftresponsive to the sensed quantity, and can provide the recombined givencomponent with the incorporated phase shift. In further examples, theseed probe light can be multiplexed between a plurality of wavelengths;and correspondingly the given component can be multiplexed betweenrespective sensing elements for the plurality of wavelengths, so as tomultiplex wherein the sensed quantity between a respective plurality ofquantities.

A disclosed method can include detecting the second probe component, thesecond conjugate component, or both to determine the phase shiftassociated with the sensed quantity. A disclosed method can also includeapplying an auxiliary phase sweep to a selected one of the second mixedlight components to sweep a fringe pattern, and determining a point ofthe auxiliary phase sweep at which a target point of the fringe patternis obtained. The determined phase shift can be evaluated as a lineartransformation of the determined point of the auxiliary phase sweep. Incertain examples, the detecting can be performed with a photosensor, andcan include applying a compensatory phase shift to a selected one of thesecond mixed light components based on feedback from an output of thephotosensor, to obtain a target fringe position at the photosensor. Thedetermined phase shift can be evaluated as a linear transformation ofthe compensatory phase shift.

In a further aspect, the disclosed technologies can be implemented as anoptical device incorporating a mode splitter, a modulator, and amode-coupling amplifier. The mode splitter is configured to split probeand conjugate modes from a pump mode within a nonlinear medium. Themodulator is coupled to receive one or more of the modes from the modesplitter at an input port, and to provide the received modes at anoutput port. A given one of the provided modes is provided with anincorporated phase shift representing a sensed quantity. Themode-coupling amplifier is situated to receive the pump, probe, andconjugate modes, including the given mode coupled from the output portof the modulator. The pump and conjugate modes undergo phase-sensitivegain within the mode-coupling amplifier. The phase-sensitive gain,averaged over values of the phase shift, and a probe gain, experiencedby the probe mode within the nonlinear medium, are in a predeterminedrelationship.

In some examples, the nonlinear medium can be a fiber with third ordernonlinear susceptibility, and the splitting can occur due topump-degenerate four-wave mixing. The splitter and the mode-couplingamplifier can employ a common gain mechanism. The incorporated phaseshift can be provided by an external fiber sensor coupled to themodulator, in the path of the given mode.

The foregoing and other objects, features, and advantages of theinvention will become more apparent from the following detaileddescription, which proceeds with reference to the accompanying figures.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a block diagram of an example optical device according todisclosed technologies.

FIGS. 2A-2C are graphs showing optical spectra at different positionswithin an example optical device according to disclosed technologies.

FIGS. 3A-3B are illustrations of four-wave mixing processes employed insome embodiments of the disclosed technologies.

FIG. 4 is a block diagram illustrating example modulator configurationsaccording to the disclosed technologies.

FIG. 5 is a graph illustrating output power of a detected lightcomponent as a function of phase shift.

FIG. 6 is a block diagram illustrating a first technique of detecting aphase shift according to the disclosed technologies.

FIG. 7 is a block diagram illustrating a second technique of detecting aphase shift according to the disclosed technologies.

FIG. 8 is a block diagram illustrating a third technique of detecting aphase shift according to the disclosed technologies.

FIG. 9 is a block diagram illustrating a multiplexed device according tothe disclosed technologies.

FIG. 10 is a hybrid diagram including a flowchart illustrating anexample method according to the disclosed technologies.

FIG. 11 is a flowchart illustrating additional features of some examplemethods according to the disclosed technologies.

FIG. 12 is a flowchart illustrating an example detection methodaccording to the disclosed technologies.

FIG. 13 is a flowchart illustrating another example detection methodaccording to the disclosed technologies.

FIG. 14 is a block diagram of an optical sensing system according to thedisclosed technologies.

FIG. 15 is a diagram of an airborne optical sensing system according tothe disclosed technologies.

FIG. 16 is a diagram of a downhole optical sensing system according tothe disclosed technologies.

FIG. 17 illustrates a generalized example of a suitable computingenvironment in which described embodiments, techniques, and technologiespertaining to a disclosed nonlinear optical device can be implemented.

DETAILED DESCRIPTION Introduction

Fiber sensors can be used in a wide range of applications, ranging fromin-flight gyroscopes, to monitoring in rugged environments such as oilwells and nuclear power plants, to detection of gravity waves. Fibersensors can be used to detect acoustic waves, temperature, mechanicalstrain, or chemicals. Increasingly, photolithography, epitaxy, andrelated technologies are being deployed to develop optical systems asphotonic integrated circuits (PIC). Both fiber and PIC technologiesoffer advantages of mechanical stability, system simplicity (e.g. lowcount of optical devices in a practical system), and ready integrationwith other fiber or PIC devices, especially compared with prior systemsemploying ⁸⁵Rb vapor and geometric optics. PIC in particular can be verycompact.

Many sensing applications can be limited in performance bysignal-to-noise ratio (SNR), namely the difficulty of detecting a signalthat is weak in relation to background noise. Additionally, in manytraditional signal chains, each successive component adds its own noisefigure, meaning that SNR can progressively deteriorate as the signal isamplified and processed.

Parametric amplification can provide nonlinear gain, so that a signal 3dB above a noise floor can be amplified by a greater amount than thenoise, meaning that SNR can actually be increased. Because signal+noisecan be greater than noise by itself, an increase in SNR can be had evenif the signal is buried well below the noise floor. Conventionally, SNRcan often be limited by shot noise, where a fractional error in ameasurement can be proportional to N^(−0.5) for N detected photons.Through nonlinear amplification, it becomes possible to operate withscaling between N^(−0.5) and the ultimate Heisenberg limit N⁻¹. Theability to operate beyond the shot noise limit is sometimes termedquantum enhancement, and is sometimes described as cancellation ofcorrelated noise. The improved SNR can exceed that of any linearinterferometer and can enable previously infeasible measurementapplications. In some examples of the disclosed technologies, nonlineargain can be provided by four-wave mixing, amplifying probe and conjugatesidebands of a pump wavelength.

However, nonlinear amplifiers can have their own limitations.Particularly, competing nonlinear processes can significantlydeteriorate SNR, visibility, sensitivity, or another figure of merit. Inother words, nonlinear amplification can pull a signal out ofpre-existing noise, but could simultaneously introduce vastly greaternoise through a competing nonlinear process. Some examples of competingprocesses can include self-phase modulation (SPM) which can lead tosuper-continuum generation, cross-phase modulation (XPM), stimulatedBrillouin scattering (SBS), or stimulated Raman scattering (SRS).Nonlinear process can also saturate. Thus, careful design of a nonlinearinterferometer can be required to optimize performance: it can beinsufficient to merely maximize gain of a desired nonlinear process.

Particularly, the present authors have discovered that for a particularclass of two-stage nonlinear interferometers, superior performance canbe achieved by balancing. In simplified terms, an unequal gaindistribution between the two stages means that the higher gain stage canbe more susceptible to competing deleterious nonlinear effects, limitingperformance either directly or indirectly. For this reason, gainbalanced stages can offer best overall gain, best SNR, best sensitivity,best fringe visibility, or best performance according to some otherfigure of merit, among competing system designs. The authors haveconducted experiments, verified noise performance, and confirmed theirresults with simulations, as described further herein.

Embodiments of the disclosed technologies can combine gain balancingwith the advantages of lightguide optics and nonlinear amplification toachieve high-sensitivity, low-complexity, and compact instruments thatenable or advance many optical sensing applications. Such instrumentscan be well-suited for room temperature or elevated temperatureoperation, and challenging environments with vibration, electromagneticinterference, dirt, contamination, remote access, or various kinds ofloss: lossy environments can be mitigated by the guided optics, whileintrinsic optical path losses can be mitigated by the SNR enhancement.

Terminology

To facilitate review of the various embodiments, the followingexplanations of terms are provided. Occasionally, and where clear fromthe context, a term may also be used in a different meaning.

As used herein, the term “airborne” refers to any apparatus installed inan aircraft.

As used herein, an “aircraft” refers to a man-made apparatus capable ofcontrolled flight through air or space. Aircraft can include airplanes,airships, drones, gliders, helicopters, or satellites. A baseball offersno capability for controlling flight once in flight and would not beconsidered an aircraft. However gliders, with movable flaps, and somemissiles, with engine control, can be regarded as aircraft.

As used herein, “amplification” can refer to a process that increasesthe power of an optical or electrical signal, or to the ensuing gain insignal magnitude.

As used herein, an “amplifier” is a device for increasing the power ofan optical or electrical signal. Some amplifiers can be generally linearwithin their normal operating conditions, meaning that doubling themagnitude of an input signal (measured as power, electric fields,voltage, or current) can double the magnitude of an output signal(measured similarly). Common electrical signal amplifiers describedherein can be linear amplifiers. Some amplifiers can be nonlinear withintheir normal operating conditions, for which a doubling of input signalmagnitude more than doubles the output signal magnitude. Common opticalsignal amplifiers described herein can be nonlinear parametricamplifiers based on four-wave mixing. Other nonlinear amplifiers canexhibit saturation behavior, where a doubling of input signal magnitudecan yield an increase in output signal magnitude by less than a factorof two. An optical signal amplifier can provide employoptical-electrical-optical (O/E/O) conversion to provide gain in theelectrical domain. As used herein, a “parametric” amplifier providesoptical amplification through a nonlinear process, such as four-wavemixing.

As used herein, an “arrayed waveguide grating” (AWG) is an opticaldevice incorporating an array of optical waveguides by which the AWGprovides wavelength dependent performance. Common AWGs can be planardevices, and can be used for multiplexing, demultiplexing, or filtering.

As used herein, the term “average,” without qualification, refers to anarithmetic mean. The average can be over a finite set of items, over afinite range, or over a period of a periodic function. Where “average”is used to describe a feature of an example of the disclosedtechnologies, other central measures can alternatively be used,including a geometric mean, a harmonic mean, a weighted mean, a median,or a mode.

As used herein, a “circuit” is an electrical circuit, i.e. an apparatuswithin which electrical charge can move. Some common circuits performfunctions on signals.

As used herein, a “circulator” is a non-reciprocal optical device havingat least three ports. Light of a given wavelength entering at port #1can primarily emerge at port #2, however light of the given wavelengthentering at port #2 does not primarily emerge at port #1. Often, lightentering at port #3 can primarily emerge at port #1.

As used herein, “coherence” refers to a fixed phase relationship betweenan electric field of light at one space-time point and anotherspace-time point. Temporal coherence refers to the electric field phaseat one space-time point being determinate from the electric field phaseat the same spatial position at a different time. Spatial coherence canrefer to transverse spatial coherence, namely the electric field phasebeing predictable in a direction transverse to the direction ofpropagation. Single-mode lightguides commonly provide spatial coherence.Some examples of the disclosed technology employ light modes havingtransverse spatial coherence throughout at least nonlinear interactionregions. Some examples of the disclosed technology provide temporalcoherence over a slippage time (e.g. due to chromatic dispersion) overthe entire nonlinear interaction regions.

As used herein, “component” refers to a component of light. Lightpropagating in a medium can include photons or waves with varyingproperties including frequency (equivalently, wavelength), polarizationstate, direction of propagation, spatial structure, or temporalstructure. A component is any portion of the light in the medium that isdistinguishable from or separable from other components based on thevarying property. In disclosed examples, components can have differentfrequency bands, sometimes labeled as probe, pump, or conjugatecomponents. Generally, a component can retain its identity throughamplification, phase shift, transiting optical devices, or some otheroptical transformations. However, sometimes a parent component can besplit into one or more child components distinct from their parent, ortwo or more distinct components can sometimes be combined into a singlecomponent. The term “mode” is sometimes used synonymously withcomponent; however, mode can also refer to e.g. a mode of operation(reflection mode, transmission mode) or as a statistical measure. Twocomponents or modes of light can be spatially distinguished, e.g. abeamsplitter can separate light into a forward propagating mode and a90° deflected mode. Components can be distinguished by frequency, e.g.co-propagating probe, pump, and conjugate modes in a lightguide can havesubstantially separate frequency bands and can be distinguished thereby.In other examples, components can be distinguished by other parameters,such as polarization state, direction of propagation, or temporalprofile. As used herein, “mode-coupling” refers to any nonlinear opticalprocess in which two different components (modes) of light interact.

In disclosed examples, nonlinear interaction between a pump componentand a sideband component can give rise to a light component dubbed a“conjugate” component that is at an image frequency, particularly wherethe pump frequency is the average of the sideband frequency and theconjugate frequency.

As used herein, a “coupler” or “optocoupler” is an optical device thatcouples a portion of light from one lightguide to another lightguide. A50-50 coupler has at least three ports; optical power received at port 1results in 50% each emerging from ports 2 and 3. A coupler can be areciprocal device, but this is not a requirement. Some couplers canoffer wavelength-insensitive performance over an operating band ofwavelengths, but this is not a requirement. Other couplers can offerwavelength-selective performance, such as an add-drop multiplexer (ADM).

As used herein, “feedback” refers to coupling an output of a device insuch a way as to influence an input to the same device.

As used herein, a “fiber” or “optical fiber” is a flexible lightguidehaving a longitudinal extent and a narrow generally uniformcross-section with a transparent core through which light can bepropagated along the length of the fiber. Some fibers have a glass core.A fiber that can support a single propagating mode (with possiblymultiple polarization states) in a given direction along the fiber isdubbed a “single mode fiber” (SMF). Fibers can be manufactured with awide range of optical properties to make them suitable for particularuses. A fiber type of interest in this disclosure is “highly nonlinearfiber” (HNLF) having a gamma factor (γ) of at least 5, and often about9, for example 9±1, measured in W⁻¹km⁻¹. HNLF can be germanium-dopedsilica fibers. For short lengths, parametric amplifier gain can scale asγPL, for pump power P and length L. Other fiber types includedispersion-shifted fibers, dispersion compensating fibers, andpolarization maintaining fibers. Optical fiber can be fabricated asoptical devices in which a functional characteristic is integratedwithin the optical fiber. A fiber Bragg grating can be such a device,embedding a longitudinal grating within a fiber to providewavelength-selective transmission or reflection properties.

As used herein, “four-wave mixing” is a nonlinear optical processcoupling four photons or, equivalently, four light waves. In examplesdescribed herein, three existing photons can interact to give rise to anew fourth photon. In other examples, two existing photons can generatetwo new photons. Of interest herein is “pump-degenerate” four-wavemixing, in which two similar pump photons, at a pump wavelength,interact with a third probe photon, in a pump sideband, to form a newfourth photon in either the pump wavelength range or a conjugatewavelength range. Four-wave mixing can be phase sensitive, andaccordingly four-wave mixing can be used to provide phase sensitiveamplification in a nonlinear medium. Commonly, four-wave mixing can relyon third-order nonlinear susceptibility χ⁽³⁾ for nonlinear couplingbetween four photons.

As used herein, a “fringe” is a detection of a phase-sensitivecombination of two or more optical signals. A fringe can be spatiallydiscernible, as in a double-slit experiment; alternatively a fringe canbe temporally discernible, as when one of the combined optical signalsis swept in phase; however, neither of these are required. One or morediscernible fringes can form a fringe pattern, having an alternatingsuccession of dark and bright fringe points. Alternatively, a fringe canbe implicit, as when a detected optical signal represents a single pointof a spatial or temporal fringe pattern.

As used herein, “gain” refers to an amount of amplification of a signal.Where used without qualification, gain of a light signal can be definedas output power divided by input power. For example, probe gain can bethe ratio of output power of a probe light component to input power ofprobe light; both input and output probe power can include seed probepower. Where used without qualification, gain of an electrical signalcan be defined as the ratio of output voltage (or current) to inputvoltage (or current).

As used herein, a “gyroscope” is an instrument for measuring ormaintaining orientation or angular velocity. An optical gyroscope canincorporate a fiber sensor having the phase of transmitted lightsensitive to angular velocity of the sensor, e.g. by the Sagnac effect.

As used herein, a “hydrophone” is an instrument for measuring acousticwaves or other pressure waves in water or another fluid. An opticalhydrophone can incorporate a fiber sensor would on a drum. An incidentpressure wave can cause corresponding oscillations in the drum diameter,which can manifest as strain in the fiber and a measurable change in itspropagation constant and in the phase of transmitted light.

As used herein, an “interferometer” is an optical apparatus which usesphase relationships between light components to make a measurement. Someinterferometers described herein can be classified as SU(1,1) devices,based on having component transformations according to an SU(1,1) Liegroup.

As used herein, a “lamp” is a source of light, which can be a transducerfrom a source form of energy into light energy. The source form ofenergy can itself be light energy, can be another form ofelectromagnetic or electrical energy, or can be another form of energy.

As used herein, a “laser” is a lamp that operates by coherent stimulatedemission of radiation in a cavity. The light from a laser commonly has ahigh degree of temporal and spatial coherence. Laser types include solidstate lasers, diode lasers, dye lasers, gas lasers, and free electronlasers. Lasers can be configured in many different ways to achievedesirable properties such as wavelength stabilization, pulsed operation(including mode-locked), or wavelength tunability. Although lasers canbe convenient lamps with satisfactory coherence properties, the use oflasers is not a requirement. Alternative examples of the disclosedtechnologies can use lamps with a lower degree of coherence, such as asuperluminescent diode (SLD).

As used herein, “light” refers to propagating electromagnetic energyhaving spectral content between about 30 THz (terahertz) and 3 PHz(petahertz). This frequency range corresponds to free-space wavelengthsof about 100 nm to about 10 μm. Frequencies and wavelengths can be usedinterchangeably in this disclosure. Particularly, light is not limitedto the visible portion of the electromagnetic spectrum (about 400 nm to800 nm). In some embodiments, light between 1200 nm and 1700 nmwavelength can be used, for compatibility with commercially availablefiber, light sources, and other devices. Although light described hereincan often be guided within media having refractive index n>1, thewavelengths ascribed to such light refer to the free space wavelengths,as is common in the art.

As used herein, a “lightguide” is a structure in which light canpropagate with spatial confinement in at least one dimension. Commonlightguides described herein have a longitudinal axis along with lightcan propagate, with substantial confinement in both transversedirections, such lightguides can be termed “axial lightguides.” Axiallightguides can commonly be fiber (such as glass fiber) or planarwaveguides (commonly silica) formed on a photonic integrated circuit(PIC). Other lightguides such as an arrayed waveguide grating (AWG) canbe planar structures supporting spreading in one transverse dimensionwithin the plane, with confinement in another transverse dimensionperpendicular to the plane. Some axial lightguides can be fabricatedinto or coupled with structures supporting purposeful partial loss ofconfinement in one or both transverse dimensions; optical couplers canbe examples. Lightguides can be free of alignment issues, can provideinherently stable geometry, can easily provide spatial overlap ofmultiple components as required for nonlinear interactions, and can bereadily deployed with long path lengths, even in a compact volume.

As used herein, a “linear transformation” is a transformation from aninput quantity (x) to an output quantity (y) of the form y=A·x+B, whereA and B can be constants. The term encompasses piecewise lineartransformations, where A=A1 and B=B1 for a segment x∈(x1, x2) and A=A2,B=B2 for a segment x∈(x2, x3). Output y need not be continuous at x=x2.Linear transformation of phase is of interest herein. Some lineartransformations of phase can be piecewise linear transformations, andcan have A1=A2 across a segment boundary; B and y jump by 2π (orequivalently 360°) at the segment boundary.

As used herein, two quantities can be said to “match” if values of eachare equal to within a tolerance. Without qualification, the term matchcan be understood to have a tolerance can be 10% for any magnitudequantity or ratio of such magnitudes, whether measured in linear orlogarithmic units (10% in power being about 0.4 dB), or a tolerance of5° (about 0.1 radian) in phase. Other phase tolerances can be 30°, 20°,10°, 2°, 1°, 0.5°, 0.2°, or 0.1°. Other magnitude tolerances can be0.1%, 0.2%, 0.5%, 1%, 2%, 5%, 20%, 50%, or 0.1 dB, 0.2 dB, 0.5 dB, 1 dB,2 dB, or 3 dB.

As used herein, a “medium” is a material through which light canpropagate. The transmissive material of a lightguide can be a medium.

As used herein, a “modulator” is an optical device that couples one ormore components of light from an input port to an output port, with achange in optical property applied to at least one of the components. Adifferential modulator transports two or more components of light frominput to output, with a change in optical property applied to onecomponent, with the same change not being applied to a second component.In some examples, the changed optical property can be the phase of aselected light component; the phase of one light component can bedifferentially modulated with respect to the phase of other components.

As used herein, a “monitoring system” refers to one or more apparatusesthat are configured to detect, measure, report, or record one or moreenvironmental or operational parameters.

As used herein, “multiplex” refers to combination of two or more opticalcomponents in a single lightguide. Conversely, “demultiplex” refers toseparation of two or more optical components from within a lightguide.Often, multiplexing and demultiplexing can occur in the spatial domain,e.g. two modes can be spatially separated, but this is not arequirement. Multiplexing or demultiplexing can occur in another domain,such as a temporal domain, or in more than one domain. A device fordemultiplexing is sometimes dubbed a “splitter,” while a device formultiplexing is sometimes dubbed a “recombiner” or just “combiner”.

As used herein, a “nonlinear” material or device is one whose intendedbehavior relies on a nonlinear process or nonlinear material property. Alinear process or property is one where the magnitude of a response oroutput is linearly proportional to the magnitude of a stimulus or input.A nonlinear process or property is a process or property which is notlinear. To varying extents, many materials or devices have both linearand nonlinear characteristics. In a linear material or device, nonlinearaspects can generally be undesirable, while in a nonlinear material ordevice, at least one nonlinear aspect can be important for intendedperformance. The same material or device can be linear or nonlineardepending on its use. A nonlinear material or device can have multiplenonlinear properties, some of which can be responsible for its intendedbehavior, while others can be undesirable.

As used herein, an “optical add-drop multiplexer” (OADM) is an opticaldevice having at least three ports: an input port, an output port, andone or more side ports. Of multiple wavelengths entering the device atthe input port, one or more selected wavelengths can be dropped out aside port, while remaining wavelengths (excluding the droppedwavelengths) exit the device at the output port. Concurrently, one ormore auxiliary light components can be added from a side port, alsoexiting at the output port. Commonly, the dropped wavelengths and theadded wavelengths can be the same, but this is not a requirement.Commonly, all dropped wavelengths can be routed out a single side port,but this is not a requirement, and similarly for added wavelengths.Commonly, side ports for dropping and adding can be separate, but thisis not a requirement. With an integrated circulator, a single OADM sideport can be used to add and drop a given wavelength.

As used herein, an “optical sensor” is an optical device formed of anoptical medium in which a property of light in the medium is changedwhen an external environmental parameter varies. In an “intrinsic”optical sensor, the environmental parameter variation causes ameasurable change in an optical property of the medium (for example,refractive index, polarization coupling, opacity, or nonlinearsusceptibility) and can be distinguished from an “extrinsic” sensor forwhich the light is changed outside the optical medium (for example bylight scattering). The intrinsic-extrinsic distinction is independent ofthe distinction between an “internal” sensor that can be integratedwithin a modulator, and an “external” sensor that can be coupled to oneor two ports of a modulator. A “fiber sensor” is an optical sensorhaving a fiber as the optical medium. Optical sensors can operate intransmission mode, having at least two ports, or can operate inreflection mode, having at least one port.

As used herein, a “path” refers to a track in space, generally acurvilinear, straight, or segmented line, followed by a component oflight. Two or more components of light can share a path, in part or inentirety. In a lightguide, a path generally follows an axis of thelightguide.

As used herein a “petrochemical access shaft” refers to a shaft belowthe earth's surface used for recovering or transporting oil, gas, oranother petrochemical fluid. Common petrochemical access shafts caninclude oil wells, gas wells, or fracking wells.

As used herein, “phase” denotes a position on an oscillatory phenomenon.The oscillatory phenomenon can be a light wave, and the position can bean angular argument of a sinusoidal function describing an oscillatoryelectric field of the light wave. For example, the electric field of alight wave propagating in the +z direction in a medium can beproportional to cos(2πft−2πz/λ+φ), where f is frequency, λ is thewavelength in the medium, t is time, z is coordinate position in the zdirection, and φ is a phase offset. By convention, the phase can betaken as the parenthetical term, and can be expressed in radians,degrees, or another angular measure. At a given coordinate z=z₀, phaseincreases with time. At a given time t=t₀, phase decreases in thedirection of propagation. At a given space time point (z₀, t₀), phaseincreases as φ increases.

As used herein, a “target phase” is a position of an oscillatoryphenomenon at which it can be desired to operate an apparatus or make ameasurement. Because phase can be related to fringes, a target phase canbe a dark fringe point, a bright fringe point, a midpoint, or anintermediate point having maximum slope. The choice of target phase candepend on a dominant noise mechanism in a given application.

As used herein, “phase-sensitive amplification” refers to a gain processin light having two or more components, in which the amount of gainexperienced by one component can be dependent on a relative phase amongthe light components. The terms phase-sensitive amplification orphase-sensitive gain encompass cases where the gain is less than unityand a component loses energy, sometimes dubbed “deamplification,” suchas at or near a dark fringe point.

As used herein, “phase shift” refers to a change in a relative phase ofa light wave at one spatial point and time relative to a reference pointat a fixed time offset. For example, if the phase of a pump component is+30° at an entrance to a phase-sensitive amplifier, relative to the exitwindow of a pump laser, and then becomes +35° at the amplifier entrance(e.g. responsive to a fiber sensor detecting temperature change), thenthe pump component has experienced or incorporated a phase shift of35°−30°=5°.

As used herein, a “phase shifter” is an optical device that imposes aphase shift on one or more light components transiting the device.

As used herein, a “photodetector” is a device that receives a lightsignal and outputs a measurement of that light signal, or arepresentation of such a measurement.

As used herein, a “photosensor” is a transducer that converts a lightsignal into an electrical signal or into some other form of signal.Photodiodes, including avalanche photodiodes, and phototransistors canbe examples of photosensors.

As used herein, a “probe” refers to a light component that canparticipate in a nonlinear mixing process. In some examples, the probecan be amplified by nonlinear amplification including phase-sensitiveamplification, can be transformed by a modulator or an optical sensor,or can be detected by a detector such as a phase sensitive detector. Theprobe component can include both seed light and probe light obtainedthrough nonlinear amplification. A probe can participate in nonlinearamplification within a restricted spatial or temporal extent, but cannonetheless be considered a probe over its entire extent.

As used herein, a “pump” refers to a light component that canparticipate in a nonlinear amplification process to transfer its ownpower into another component. A pump can provide nonlinear amplificationwithin a restricted spatial or temporal extent, but can nonetheless beconsidered a pump over its entire extent.

As used herein, “seed” refers to a light component injected into anoptical amplifier, to be amplified therein.

As used herein, “sense” means to convert a physical or chemicalparameter into an optical or electrical signal. In some examples, thesensed parameter can be an environmental parameter, and the opticalsignal can be a phase shift of a light component.

As used herein, a “sensing system” is an apparatus for making ameasurement of a sensed parameter.

As used herein, “susceptibility” χ refers to a tensor property of amaterial relating vector electric field E and vector polarization P, viaP=χE. Of interest in this disclosure is a third-order nonlinearcomponent of susceptibility which can enable four-wave mixing, viaP₄=χ⁽³⁾E₁E₂E₃. While χ⁽²⁾ materials can also exhibit χ⁽³⁾, they can alsohave dominant nonlinear effects due to χ⁽²⁾. Accordingly, in someexamples, nonlinear materials whose principal nonlinear susceptibilityis χ⁽³⁾ can be preferred.

As used herein, “sweep” refers to a continuous modulation of a signalparameter, such as phase.

As used herein, a light component that enters an optical device andleaves the optical device can be said to “transit” the device. The lightcomponent can transit the device in reflection mode (emerging from theentrance port), in transmission mode (emerging from a different port),or in a combination of modes.

As used in this disclosure, “visibility” of a fringe is a measure ofdiscernibility between dark and bright fringe positions. Visibility Vcan be defined by an equation V=(Pmax−Pmin)/(Pmax+Pmin), that is, theratio of fringe amplitude (in power units) to median power, where Pmaxand Pmin represent optical power at the bright and dark fringe pointsrespectively.

First Example Device

FIG. 1 is a block diagram 100 of an example optical device 120 accordingto disclosed technologies. Several insets in FIG. 1 show properties ofoptical signals and other parameters to assist with the description ofFIG. 1. Optical device 120 includes nonlinear lightguides 130, 170coupled by a modulator 150. Nonlinear lightguide 130 can generate probeand conjugate sidebands 132, 136 of pump light 124, 134 with adeterminate phase relationship. Modulator 150 can introduce a phaseshift 155 on one or more received components of light 153A, 153B.Nonlinear lightguide 170 can provide phase-sensitive amplification 175of second probe and second conjugate light components 172, 176. Thus,the developed power of second probe 172 or second conjugate 176 lightcomponents at the output of lightguide 170 can depend on the phase shift155 introduced at modulator 150, and optical device 120 can be used as ameasuring instrument.

Nonlinear lightguide 130 can be coupled to lamps 112, 114 to receiveseed probe light 122 and pump light 124 respectively through optocoupler116. Through a nonlinear process, the pump light 124 and seed probelight 122 can interact to amplify the seed probe light 122 into probelight 132. Conjugate light 136 can also be concurrently generated withinthe nonlinear lightguide 130. The pump light 124, 134, the probe light132, and the conjugate light 136 can be spatially and temporallyoverlapping, and can be regarded as components of mixed light 138 withinor at an output of nonlinear lightguide 130.

The probe gain 135 can be defined as a ratio of output power of probelight 132 to input power of seed probe light 122. The probe gain 135 canbe dependent on length 131 of nonlinear waveguide 130.

Modulator 150 can receive a given component 153A of the mixed light 138from nonlinear lightguide 130. With incorporation of a phase shift 155,given component 153B can be forwarded to nonlinear lightguide 170. Invarying embodiments, the given component 153A can be a probe lightcomponent 132, a conjugate light component 136, or a pump lightcomponent 134. In some embodiments, an optical sensor 160 can be coupledto modulator 150 to provide the phase shift 155 representative of aphysical or chemical quantity such as pressure, temperature, etc. Othercomponents of mixed light 138 can pass through modulator 150 withoutexperiencing the phase shift 155, so that the determinate phaserelationship among the components of mixed light 138 can be changeddependent on a sensed quantity.

Nonlinear lightguide 170 can be coupled to receive at least thephase-shifted given component of light 153B from modulator 150.Nonlinear lightguide 170 can also be coupled to receive othercomponents, either through modulator 150 or from an alternate path. Forexample, if the given component 153A, 153B is probe light 172, then theother components include pump and conjugate light 174, 176, andsimilarly if the given component 153A, 153B is pump light 174 orconjugate light 176. Thus, nonlinear lightguide 170 receives mixed light178 comprising probe light 172, pump light 174, and conjugate light 176,one of which can be the phase-shifted given light component 153B.Through a nonlinear process, pump light 174 can amplify probe light 172and conjugate light 176, with phase-sensitive gain 175 dependent onphase shift 155. The phase-sensitive gain 175 can be averaged over arange of phase shifts 155 (e.g. 0 to 2π) to obtain averagedphase-sensitive gain 177. Both phase-sensitive gain 175 and averagedphase-sensitive gain 177 can be dependent on length 171 of nonlinearwaveguide 170. Due to the phase-sensitive gain 175, the power of one ormore components output from amplifier 170 can be dependent on the phaseshift 155, and optical device 120 can be used as an interferometer.

As described herein, superior performance can be obtained when one orboth of lengths 131, 171 are selected so that the averagedphase-sensitive amplification 177 matches the probe gain 135.

Outputs of nonlinear lightguide 170 can be coupled to a photodetector180 to detect one or both of amplified probe light 172 or amplifiedconjugate light 176, and measure the phase shift 155 therefrom.Exemplary measurement techniques are described herein.

Numerous of the blocks depicted in FIG. 1 can be coupled to acomputer-implemented measurement and control system (not shown)incorporating one or more computing environments with one or morecontrollers and one or more data acquisition subsystems.

Many variations are possible, including without limitation thosedescribed herein. For example, optical device 120 can be extended toincorporate one or more additional items as shown in FIG. 1 or asdescribed elsewhere herein, without limitation. A seed lamp 112 canprovide a determinate probe component, free of vacuum noisefluctuations. However, some examples can omit seed lamp 112, allowingthe probe and conjugate to be spontaneously generated.

The average phase-sensitive gain can be calculated over a range ofphases, which can vary between examples. In some examples, the averagephase-sensitive gain can be calculated over all phases (0 to 2πradians), while in other examples, the average phase-sensitive gain canbe calculated over a narrower range accessible during operation of asystem, such as within 30° or within 30° of a target phase point.Particularly, in an example configuration employing feedback control,such as described with reference to FIG. 7, the deviation from a targetphase point during normal operation can be quite small, and the averagephase-sensitive gain can be an average of a single value, namely thephase-sensitive gain at the target phase point.

In varying examples, a nonlinear lightguide (e.g. lightguide 130 or 170)can be an optical fiber or a waveguide on a photonic integrated circuit(PIC), sometimes dubbed planar lightwave circuit (PLC). A PIC embodimentof device 120 can be a chip scale device. A nonlinear lightguide can bea single-mode (SM) guide supporting a single propagating mode of probe,pump, or conjugate light components. A nonlinear lightguide 130, 170 canhave an effective third-order susceptibility χ⁽³⁾ and can lack aneffective second-order susceptibility χ⁽²⁾. A gain process in anonlinear lightguide can be four-wave mixing, e.g. pump-degeneratefour-wave mixing. Both nonlinear lightguides 130, 170 can have matchingcross-sectional structure or matching composition. In some examples,nonlinear lightguides 130, 170 can be formed of telecom single-modefiber for operation in the L band (1565-1610 nm), exploiting a weak χ⁽³⁾nonlinearity over suitable fiber lengths.

The lamp 114 producing pump light 124 can be a pulsed laser, e.g. amode-locked laser. Controller 115 can be coupled to pulsed laser 114,for example to provide active mode-locking. The lamp 112 producing seedprobe light 122 can be a continuous-wave (CW) laser. Controller 113 canbe coupled to CW laser 112, for example to provide time-multiplexedwavelengths, or wavelength stabilization.

While components of mixed light 138, 178 can follow a same path withinnonlinear waveguides 130, 170, modulator 150 can be implemented with asplitter and a recombiner to separate the spatial paths of variouscomponents of mixed light 138. Particularly, the spatial path of a givencomponent 153A can be routed through an optical sensor 160 to develop aphase shift 155 representative of a sensed quantity. As shown in FIG. 1,optical sensor 160 can be an external sensor operating in transmissionmode, receiving the given component of light 153A at a first modulatorport, transporting the given component, and returning the givencomponent 153B, with phase shift 155 applied, to a second modulatorport. Sensor 160 can incorporate a length of optical fiber. In otherexamples, the external sensor 160 can be a reflection mode sensor, suchas a fiber Bragg grating (FBG), or the optical sensor 160 can beco-housed with, or integrated within, the modulator 150.

Example Spectra

FIGS. 2A-2C are graphs showing optical power spectra at differentpositions within an example optical device according to disclosedtechnologies. FIGS. 2A-2B are indicative of spectra at the input andoutput of nonlinear lightguide 130 shown in FIG. 1, while FIG. 2C isindicative of an optical power spectrum at the input of nonlinearlightguide 170.

Beginning with FIG. 2A, graph 210 shows average power recorded by anoptical spectrum analyzer (OSA) over a 2 GHz resolution bandwidth, as afunction of the frequency of electromagnetic radiation. The seed probelight appears as a narrow spike 212 with amplitude +12 dBm (about 16mW). For the illustrated example, the seed light was provided by astabilized CW laser 112 with bandwidth well below 1 GHz. Consequently,the spectral peak 212 would not be significantly changed by a reductionof OSA resolution bandwidth to 1 GHz. The pump light appears as abroader spectral profile 214 having a peak of about −27 dBm. Because thespectral profile 214 can be broad compared to the resolution bandwidth,a reduction of resolution bandwidth by half, would reduce the peak powerby about half, to about −30 dBm. For the illustrated example, the pumplight was provided by a mode-locked pulsed laser 114 having a duty cycleof about 10⁻⁴. Because the OSA reports average power, the instantaneouspump power during a laser pulse can be about 40 dB higher than shown,i.e. with a peak of about +13 dBm (20 mW) in a 2 GHz resolutionbandwidth. Taking into account the bandwidth of the pump radiation, theinstantaneous pulsed pump power can be about 10 W in the illustratedexample, well above the instantaneous seed probe power.

Turning to FIG. 2B, graph 220 shows evolved optical spectra throughfour-wave mixing in nonlinear lightguide 130. Pump and seed probe lightcouple to create probe light, centered at the seed probe frequency, andconjugate light at an image frequency. Relative to FIG. 2A, spectralpeak 224 of the pump can be seen to have diminished, as pump power isconverted to probe light 223 and conjugate light 226. From theperspective of gain calculation, the seed probe can be regarded as partof the probe light, i.e. probe light can include photons from seed laser112 (in narrow peak 222) as well as photons formed by four-wave mixing(broader profile 223). Furthermore, as the probe power builds along thenonlinear lightguide 130, four-wave mixing between pump 224 and probeseed 222 can be supplemented by four-wave mixing between pump 224 andprobe 223, or by four-wave mixing between pump 224 and conjugate 226.Four-wave mixing processes are described further herein.

In some embodiments, the mixed light inputted to the second nonlinearlightguide 170 can have substantially similar spectrum to that shown inFIG. 2B. Although one of the light components can undergo a phase shiftbetween input and output of the modulator, the power spectra can remainsubstantially unaffected. In other embodiments, it can be desirable tofilter out the seed probe light 222 from the total probe light (222, 223together). For example, a four-wave mixing process with the seed can addDC (that is, phase-independent) white noise and reduce the fringecontrast; filtering out the seed can improve fringe contrast. In otherexamples, a phase shift 155 can be developed in a resonant device suchas a fiber Bragg grating, and the interaction between a resonant deviceand a broad smooth probe spectrum 223 can be more predictable withoutnarrowband interaction between a narrow seed probe spectral line 222 anda sharply resonant FBG. In other words, it can be desirable to have aprobe spectral width larger than (at least 2×, 3×, or 10× times) theresonance width, stability, or manufacturing tolerance of a resonantdevice such as an FBG sensor. A notch filter can be incorporated, forexample in the modulator 150, to provide narrow-band attenuation of seedprobe light 222.

FIG. 2C is a graph 230 showing a probe spectrum with the seed probeselectively notched out. The pump spectrum 234 and the conjugatespectrum 236 can be generally similar to FIG. 2B. However, the probespectrum 233 shows a notch, with the seed light attenuated by about 50dB in the illustration.

Example Nonlinear Mixing Processes

FIGS. 3A-3B are diagrams 310, 320 of four-wave mixing processes employedin some embodiments of the disclosed technologies. Diagrams 310, 320 aredrawn as energy diagrams relative to a ground state 301, with photonsproviding transitions to virtual energy states as shown. In FIG. 3A, twopump photons 312, 314 combine to reach a virtual energy 315 (shown as adashed line). Seed probe (or probe) photon 316 drops the virtual energyto 317, and finally conjugate photon 318 returns the process to groundstate 301. Conjugate photon 318 can be a four-wave mixing product ofpump photons 312, 314 with probe photon 316. In energy terms, thefour-wave mixing process of diagram 310 satisfies:E-conjugate=E-pump1+E-pump2−E-seed.

The light components participating in diagram 310 can have some spectralwidth, as indicated by tick marks on the associated photon transitions.The widths of the pumps 312, 314 are represented by three tick marks.The width of the seed probe 316 can be small and is represented by asingle tick mark. Finally, the conjugate 318 can be somewhat wider thanthe pumps 312, 314 owing to lack of energy correlation between the pumpphotons 312, 314.

Although illustrated with photon 316 as seed probe light, a similarprocess can occur with photon 316 as non-seed probe light, correspondingto spectral profile 223. In such a process, the spectral width of mixingproduct 318 can be somewhat greater than for the illustrated case. Asimilar process can also occur with photon 316 being conjugate light,with mixing product 318 generated in the probe spectral region, i.e.E-probe=E-pump1+E-pump2−E-conjugate. These two processes may not besignificant until the instantaneous non-seed probe power has built up tobe comparable with instantaneous seed probe power.

In FIG. 3B, a pump photon 322 and a seed probe photon 326 combine toreach a virtual energy 325. A second pump photon 324 drops the virtualenergy to 327, and finally a probe photon 323 returns the process toground state 301. The tick marks on the photons 322, 324, 326, 323represent spectral widths of the associated light components, similar toFIG. 3A. In energy terms, the four-wave mixing process of diagram 320satisfies: E-probe=E-pump1+E-seed−E-pump2. As for FIG. 3A, similarprocesses as illustrated in diagram 320 can occur with seed photon 326replaced by non-seed probe photon (from spectral profile 223) or aconjugate photon (from spectral profile 226).

Other four-wave mixing processes can occur to a lesser extent, such asnon-degenerate mixing of probe, pump, and conjugate light. In examples,the processes shown in FIGS. 3A-3B can be dominant. As probe andconjugate power build up along nonlinear lightguide 130, the similarprocesses described above can also contribute.

The pump-degenerate four-wave mixing described above can be regarded asa phase-insensitive process. The two pump photons involved can beregarded as phase coherent. The probe (including seed probe) light canbe at a different frequency than the pump, resulting in continuous phaseslip between pump and probe. In examples, the slip distance over whichpump and probe slip by one period can be on the order of microns ormillimeters, far shorter than a typical length of nonlinear lightguide130, which can be meters or kilometers. Nonlinear gain averages out overa slip distance, and builds up over the length of nonlinear lightguide130, which can be many times the slip distance.

In other examples, two independent pumps can be used forPump-1⊗Pump-2⊗Probe and similar interactions, i.e. four-wave mixing thatis not pump-degenerate.

Example Modulator

FIG. 4 is a block diagram 400 illustrating configurations of an examplemodulator 450 according to the disclosed technologies. Modulator 450 canhave an input port 451 at which mixed light 438 can be received from anonlinear lightguide such as 130 and an output port 459 at which mixedlight 478 can be coupled to a nonlinear lightguide such as 170. Withinmodulator 450, any of a variety of optical transformations can beapplied selectively to one or more light components. Here, severalexemplary transformations are illustrated and described individually forthe sake of clarity, however embodiments of the disclosed technologiescan freely combine any of these transformations on any components, alongwith additional optical transformations as are known in the art but notexplicitly described herein. Furthermore, for the sake of illustration,modulator 450 is shown with 10 separated internal light paths. However,examples of the disclosed technology can have fewer internal lightpaths, with one or more of the illustrated transformations variouslyimplemented among these light paths, in any combination.

In order to selectively operate on various light components, modulator450 can include a splitter 453 to spatially separate the variouscomponents of incoming mixed light 438, and recombiner 457 to combinevarious components into mixed guided light 478. In some examples,splitter 453 can spatially separate all components of mixed light 438from each other, for example by an arrayed waveguide grating (AWG).Similarly, recombiner 457 can be implemented with an AWG. In otherexamples, only select components for which optical transformations areimplemented can be spatially extracted, separately or together, whileother components can flow directly from input 451 to output 459. Forsuch examples, an optical add-drop multiplexer (OADM) can be used toimplement splitter 453 and recombiner 457. Path 455 is an examplestraight through path, which can be wholly contained within a combinedimplementation of splitter 453 with recombiner 457 such as an OADM, orwhich can be implemented as a dedicated lightguide between separateddevices 453, 457 such as a pair of AWGs.

Transformations of interest for phase sensing instrumentation includephase shifts dependent on a physical or chemical quantity, applied toone or more light components. Intrinsic lightguide sensors can be used,being sensitive to temperature, pressure, angular rotation, electricalcurrent, other physical parameters, or a chemical compound. Such sensorscan be implemented in fiber or in a PLC waveguide. Severalconfigurations are shown in FIG. 4. In one configuration, a sensor 441can be incorporated within modulator 450. In another configuration,sensor ports 442, 443 can be provided for coupling with an externalsensor 444. Sensor 444 operates in transmission mode: the sensor 444receives its light component at sensor port 442 and provides the lightcomponent, with variable phase shift incorporated, back to the modulatorat sensor port 443. In other examples, it can be desirable to employreflection mode sensors 447, 448. In such a configuration, a single port446 can be provided, to which one or more reflection mode sensors can becoupled. A device 445 can be incorporated within modulator 450 so thatincident light from splitter 453 and phase-shifted light to recombiner457 can share the single port 446. The device 445 can be a coupler, suchas a 50/50 coupler, or a circulator, such as a Faraday rotator or othernon-reciprocal device. In further examples, reflection mode sensors 464,465 can be coupled to a dual-port modulator interface 461, 462 with anexternally connected circulator or coupler 463 as shown.

In addition to incorporating a phase shift from a sensor, a number ofother functions can be provided with modulator 450. Optical devices 422,424, 426, 428 illustrate several optical devices that can be implementedon a separated light path within modulator 450. Controllable phaseshifter 422 can be driven by an external controller 421 and can apply avoltage controlled phase shift on path 423. Externally controlled phaseshifts are described further herein in the context of phase measurement.In varying examples, the control signal from controller 421 can be aslowly varying signal, for example tracking variations in phase shiftintroduced by sensor 444, or the control signal can be a continuouslyvarying sweep or oscillatory signal.

Fixed phase shifter 424 can apply a fixed phase shift on path 425. Delayline 426 can provide a group delay on path 427. Filter 428 can provide anotch filter, a bandpass filter, or another filter on path 429. Althoughdevices 422, 424, 426, 428 are illustrated as integrated withinmodulator 450, this is not a requirement. Any one or more of suchdevices can be provided external to the modulator 450 and coupledthrough ports, similar to ports 442, 443 shown for sensor 444. In someinstances, a single-port connection can be used as described inconnection with port 446.

Dispersion compensation can be provided for individual light componentson their respective light paths, as with optical delay line 426.Dispersion compensation or dispersion slope compensation can also beprovided on a combined light path by a dispersion compensator 452, whichcan include a length of dispersion compensating fiber. Dispersioncompensation can be provided on an end-to-end basis, and not limited tocompensation of dispersion of a preceding lightguide (130). Dispersioncompensation, filtering, and other transformations can be used toalleviate effects of undesirable nonlinear processes.

While some examples forward all received components of input light 438to output light 478, this is not a requirement. A component can bedropped at path 454 and another component can be added at path 456. Forexample, output from a pump source lamp can be split in two componentswith a determinate phase relationship, and these can be used toseparately pump the two nonlinear lightguides. The “X” symbol on path454 indicates a terminated optical path. A termination of an opticalpath can be absorptive, reflective, or mode-converting.

Numerous other variations are possible. For example, some sensorapplications can be suitable for differential sensing, where a positivephase shift, say, can be detected on one light component and a negativephase shift can be detected on another light component. The combinationof phase shifts can reject common mode phase shifts. Such aconfiguration can be as shown with sensors 441, 444, with both sensorsintegrated within modulator 450 as shown for sensor 441, or both sensorsexternally coupled as shown for sensor 444. The relevant phase in adisclosed phase-sensitive amplifier can be written as(2·φ₀−(φ_(P)+φ_(C))), where φ₀, φ_(P), φ_(C) are respectively the sensedphase shifts in pump, probe, and conjugate components. Accordingly, thedifferential sensing can be accomplished in a variety of ways. As afirst example, the positive phase shift can be applied to both probe andconjugate components, and the negative phase shift can be applied to thepump component. As a second example, the positive phase shift can beapplied to the pump component, and the negative phase shift can beapplied to the conjugate (or the probe) component with twice thesensitivity (e.g. twice the sensing length). For some examples, positiveand negative phase shifts can be applied to the pump and conjugaterespectively, with e.g. the conjugate sensitivity having reversed signbecause of being wound in an opposite sense. Gyroscope, hydrophone, andnumerous other measurement applications can benefit from differentialsensing.

Example Phase Scan

FIG. 5 is a graph 500 illustrating output power of a detected lightcomponent as a function of phase shift. Solid trace 510 depicts measuredpower (in nW) of the probe component as a function of phase shift (inradians) applied to the probe component. With reference to FIG. 1, theoutput power can be measured at a photodetector such as 180, and thephase shift can be applied by an optical sensor such as 160. Varyingpower can be a result of phase-sensitive gain in nonlinear amplifier170. As expected for this configuration, the phase-sensitive gain sweepsthrough one full oscillatory cycle as the probe phase is scanned by 2π(approx. 6.28) radians.

Dotted line trace 520 depicts measured power (in nW) of the probecomponent as a function of phase shift (in radians) applied to the pumpcomponent. Otherwise, the experimental configuration is similar to thatfor trace 510. In this configuration, the phase-sensitive gain sweepsthrough two full oscillations as the pump phase is scanned by 2πradians.

Phase-sensitive gain can be understood by considering, in a simplifiedmodel, electric fields of a pump wave E₀=A₀·cos(ω₀t+φ₀), a probe waveE⁻=A₁·cos((ω₀−ω₁)t+φ₁), and a conjugate wave E₊=A₁·cos((ω₀+ω₁)t). Here,E represents electric field, A is amplitude of the electric field, t istime, ω₀ is the pump frequency, ω₁ is the offset between pump and probeor conjugate sidebands. In this model, probe and conjugate waves can beassumed to have the same amplitude A₁, and the conjugate phase can beset to 0 without loss of generality. Summing the probe and conjugatewaves, E₊+E⁻=2A₁·cos(ω₀t+φ₁/2)·cos(ω₁t−φ₁/2). The first cosine termrepresents a wave at the same frequency as the pump, and the secondcosine term represents a slowly varying envelope at the sideband offsetfrequency ω₁. The nonlinear gain interaction between pump and sidebandsdepends on the relative phase between pump (phase: φ₀) and the combinedsidebands (phase: φ₁/2). The phase-sensitive gain can be twice assensitive to change in pump phase compared to change in probe phase, asillustrated in FIG. 5. A phase-sensitive gain process can generallyconform to the diagram of FIG. 3A.

Because the output power is sensitive to applied phase shift (e.g. 155),the measured output power can be used to determine the applied phaseshift. Some detection schemes are described herein. In some examples, aphase detector can be configured to determine or track a specificoperating point. Possible operating points 512, 514, 516 are marked onprobe scan trace 510.

In some examples, best phase sensitivity can be obtained at the darkfringe point 512, which can be due to rapid noise fall-off at the darkfringe point, a property of the nonlinear gain process in lightguide170. In other examples, a different operating point can be used.Operating points 514, 516 have steep gradient of power as a function ofscanned phase, and can be chosen as target operating points in suchexamples.

Also shown in FIG. 5 is the output power midway between minimum andmaximum, represented by dashed line 530. The traces 510, 520 can exhibitsome distortion relative to a harmonic-free sinusoidal waveform, whichcan be due to competing nonlinear effects having different phasedependence than the phase sensitive gain described herein.

First Example Detector

FIG. 6 is a block diagram 600 illustrating a first technique ofdetecting a phase shift according to the disclosed technologies.Nonlinear lightguides 630, 670 can be coupled by modulator 650. Similarto nonlinear lightguide 630, lightguide 630 can be configured togenerate probe and conjugate light components, e.g. by four-wavepump-degenerate mixing. Modulator 650 diverts the probe component tooptical sensor 660 where a phase shift, representative of a sensedquantity, can be applied to the probe component. Similar to nonlinearlightguide 170, lightguide 670 can be configured for phase-sensitiveamplification of probe and conjugate light components.

For the illustrated system, detector 680 can provide optical powermeasurement of the probe component, and determination of the phase shiftapplied by sensor 660 and an associated sensed variable.

Bandpass filter 681 can transmit the probe component outputted fromlightguide 670, and can block pump and conjugate components. Inalternate examples, a bandstop filter 681 can be used to drop the pumpcomponent and pass both probe and conjugate components. The transmittedcomponent can be measured by photosensor 683, which can be a photodiode(PD), avalanche photodiode (APD), or phototransistor. The resultingelectrical signal can be amplified by amplifier 685 and then input to acomputing system 690. Computing system can include a data acquisitionsubsystem 693, a computer processor 695, and a look-up table 697 whichcan store a table of sample values representing all or part of ancalibrated interferometric response curve such as 510. The output ofamplifier, representing measured power, can be digitized by dataacquisition subsystem 693 and provided to computer 695, where tablelook-up can be performed on table 697 to determine the sensed phase. Inexamples, the sensed phase can be further transformed by computer 695 todetermine a value of the underlying sensed parameter (e.g. temperatureor another environmental parameter).

Second Example Detector

FIG. 7 is a block diagram 700 illustrating a first technique ofdetecting a phase shift according to the disclosed technologies.Nonlinear lightguides 730, 770 can be coupled by modulator 750. Similarto nonlinear lightguide 130, lightguide 730 can be configured togenerate probe and conjugate light components, e.g. by four-wavepump-degenerate mixing. Modulator 750 diverts the probe component tooptical sensor 760 where a phase shift, representative of a sensedquantity, can be applied to the probe component. Similar to nonlinearlightguide 170, lightguide 770 can be configured for phase-sensitiveamplification of probe and conjugate light components.

For the illustrated system, detector 780 can provide optical powermeasurement of the probe component, feedback control to a targetoperating point, and determination of the phase shift applied by sensor760 and the associated sensed quantity.

Bandpass filter 781 can transmit the probe component outputted fromlightguide 770, and can block pump and conjugate components. Inalternate examples, a bandstop filter 781 can be used to drop the pumpcomponent and pass both probe and conjugate components. The transmittedcomponent can be measured by photosensor or electro-optical (O/E)converter 783, which can be a photodiode (PD), avalanche photodiode(APD), or phototransistor. The resulting electrical signal can beamplified by amplifier 785 and then sensed at differential amplifier789. In the illustrated configuration, a target operating point can bedefined by a voltage 787 provided to the positive input of differentialamplifier 789. The output of differential amplifier 789 can be fed backto control an auxiliary phase shifter 762 on a second light component.Auxiliary phase shifter 762 can be a voltage controlled phase shifter.

The feedback operates to adjust the auxiliary phase shifter 762 untilthe optical power detected at PD 783 matches the power at the targetoperating point (e.g. 512, 514, 516). Then, the output voltage of thefeedback amplifier 789 can be a measure of the auxiliary phase on phaseshifter 762 required to compensate for the phase shift (e.g. 155) ofsensor 760. This output voltage can be converted to the phase shift bycircuit 791. For example, a sensor phase shift of +10° in the probecomponent can be compensated by an auxiliary phase shift of −10° in theconjugate component, an auxiliary phase shift of +5° in the pumpcomponent, or an auxiliary phase shift of −10° in the probe component.With regard to the last, in some examples, the auxiliary phase shift canbe applied to the same component as the sensed phase shift. In suchexamples, the probe component provided to the lightguide 770 canincorporate two phase shifts, both the sensed phase shift representing asensed quantity, from 760, and a compensating phase shift similar tothat described for 762. The transfer function to map auxiliary phaseshift to sensed phase shift can be a linear transfer function, whichincludes piecewise linear transfer functions arranged to accommodatediscontinuities where either the auxiliary phase shift or the sensedphase shift wraps around, e.g. at 0=2π radians.

Finally, circuit 793 can be configured to convert the sensed phase shiftto a measurement of the underlying sensed quantity, via a known transferfunction of sensor 760. The measured physical quantity (or chemicalcompound) obtained at circuit 793 can be output to a computer display,output to an analog or digital meter, stored in a computer file, ortransmitted over a network to a client device.

Circuits 791, 793 can be implemented as analog or digital circuits inany combination. For example, an analog operational amplifier circuitcan provide the linear transfer function of circuit 791 to convert fromauxiliary phase shift to sensed phase shift. In another example, ananalog-to-digital converter (ADC) and a microprocessor can be configuredto provide digitization of the sensed phase and inversion of thetransfer function of sensor 760, in the digital domain, for circuit 793.Other alternatives can also be used. Varying implementations of otherdetector blocks 781-789 can also be used. For example, the feedbackamplifier 789 can be implemented in the digital domain, or a digitallycontrolled auxiliary phase shifter 762 can be used.

Furthermore, any combination of detector blocks 781-793 can beintegrated on one or more semiconductor or photonic integrated circuits,or can be packaged together. All or part of detector 780 can similarlybe integrated with the lightguides 730, 770 or other units shown in FIG.7.

Third Example Detector

FIG. 8 is a block diagram 800 illustrating a second technique ofdetecting a phase shift according to the disclosed technologies.Lightguide 830, 870, modulator 850, and optical sensor 860 can begenerally similar to those described in context of FIG. 1 or FIG. 7.Auxiliary phase shifter 862 can be functionally similar to phase shifter762, however phase shifter 862 can be integrated within modulator 850 asillustrated. Within detector 880, filter 881, PD 883, and amplifier 885can be similar to corresponding units in detector 780. Accordingly, theoutput of amplifier 885 reflects the phase-sensitive gain in nonlinearlightguide 870, dependent on the sensed phase shift of sensor 860 andthe auxiliary phase shift of phase shifter 862.

In detector 880, a free-running oscillator 865 can be used tocontinuously sweep the auxiliary phase of shifter 862. In varyingexamples, the output 867 of oscillator 865 can be a sawtooth wave (forlinear sweep of the auxiliary phase), a sinusoidal wave, or a trianglewave. Thus, the output of amplifier 885 can generally follow theperiodic oscillation of oscillator 865, with an additional phase shiftrepresentative of the sensed phase shift of sensor 860.

Phase sensitive detector 889, which can be a lock-in amplifier, can usesignal 867 as a reference input, and can measure the sensed phase shiftdirectly. Similar to circuit 793, circuit 893 can convert the sensedphase shift to a measurement of the underlying physical or chemicalquantity. As for detector 780, numerous variations are possible.Although FIGS. 7-8 have been described with the sensed phaseincorporated into a probe component, this is not a requirement. Invarying examples, the sensed phase can be alternatively be applied toconjugate or pump components, as described herein.

Example with Wavelength Multiplexing

FIG. 9 is a block diagram 900 illustrating a multiplexed deviceaccording to the disclosed technologies. Nonlinear lightguides 930, 970can be similar to those described in context of FIG. 1, and can becoupled by modulator 950. A pump lamp provides a fixed wavelength pumpinput 924 to lightguide 930. Seed probe light can be multiplexed betweenlight components 922, 923 at respective wavelengths. The inset in FIG. 9indicates the spectral positions of the light components 922-924 as afunction of frequency. The multiplexed seed light 922/923 can beprovided by a single laser with wavelength control, or can be providedwith independent sources for the two wavelengths, with seed components922/923 multiplexed using an optical shutter, switch, or other couplingarrangement. Lamps and multiplexing components are not shown in FIG. 9.

Within modulator 950, probe light components obtained from seed light922, 923 follow respective paths 952, 953, and correspondinglyincorporate sensed phase shifts from respective optical sensors 962,963. Pump and conjugate components follow path 955, which in varyingexamples can be a single path or a plurality of optical paths forrespective components.

Following phase-sensitive gain in lightguide 970, the amplified probecomponents can be separated by splitter 975, and detected by detectors982, 983. Each detector 982, 983 can employ one of the detectiontechniques described herein, or another detection technique. In someexamples, both detectors 982, 983 can share a single auxiliary phaseshifter, similar to shifter 862 of FIG. 8, on the pump component. Thedetails of detectors 982, 983 and auxiliary phase shifters are not shownin FIG. 9.

For simplicity of illustration, FIG. 9 has been described in terms of amultiplexed probe light component throughout. However, this is not arequirement, as the conjugate component mimics the multiplexed behaviorof the seed probe source and also experiences phase-sensitiveamplification in lightguide 970. Thus, one or both of detectors 982, 983can alternatively or additionally detect conjugate light, in anycombination. Independent of the detected light components, the sensedphase shift can alternatively be incorporated in a conjugate lightcomponent. That is, one or both of separated light paths 952, 953 can bea path of a corresponding conjugate light component. In any of theseconfigurations, the component in which a sensed phase shift isincorporated can be multiplexed between respective sensors 962, 963 asthe seed probe light is multiplexed. Accordingly, the sensed quantitycan be multiplexed between respective quantities detected by the sensors962, 963.

Furthermore, the illustration of FIG. 9 can be extended to more than twoseed probe wavelengths (922, 923, . . . ) and more than two separatedoptical paths (952, 953, . . . ) on which respective sensors (962, 963,. . . ) can be deployed. Multiplexing can be performed by alternatetechniques, singly or in combination. For example, optical switches orshutters can be configured to selectively direct the light path of asingle light component among a plurality of sensors.

Example Method

FIG. 10 is a hybrid diagram 1000 including a flowchart illustrating amethod according to the disclosed technologies. The method is describedwith reference to the apparatus of FIG. 1 for convenience ofillustration, however the method is not limited to such apparatus.

At process block 1010, seed probe light can be amplified by a first gainin a first nonlinear lightguide NLG1 1030 (similar to 130), to formfirst mixed light 1038 including first probe light, first pump light,and first conjugate light components. In examples, the gain can beobtained through a nonlinear process such as pump-degenerate four-wavemixing (e.g. FIG. 3). At process block 1020, second mixed light 1078 canbe provided to a second nonlinear lightguide NLG2 1070 (or 170), thesecond mixed light 1078 including second probe, second pump, and secondconjugate light components. The components of the second mixed light canhave phase relationships 1002 with the respective components of thefirst mixed light. The phase relationship for one of the components caninclude a phase shift 1055 representative of a sensed quantity. Atprocess block 1030, the second probe and second conjugate components canbe amplified in the second nonlinear lightguide 1070. The amplificationcan be phase-sensitive, and the gain experienced by second probe orsecond conjugate components can be dependent on phase relationshipsbetween probe, conjugate, and pump components as described herein. Thegains in nonlinear lightguides 1030, 1070 can have a predeterminedrelationship 1004. For example, the lengths of the first and secondlightguides 1030, 1070 can be selected so that an average of thephase-sensitive gain in the second lightguide 1070 matches gainexperienced by the probe component in the first lightguide 1030, forpump and seed power levels introduced into the lightguides 1030, 1070,and other optical parameters. In other embodiments, the gains innonlinear lightguides can have a different relationship, e.g. 2:1 or 1:2or another relationship, according to specific operating conditions ordominant confounding nonlinear effects.

In some examples, one or more components of the second mixed light canbe coupled from the first nonlinear lightguide 1030, 130 to the secondnonlinear lightguide 1070, 170 through a modulator (e.g. 150). The phaseshift 1055 can be provided by an intrinsic fiber sensor (e.g. 150). FIG.11 is a flowchart 1100 illustrating additional actions that can beperformed using a modulator (150) or an optical sensor (160). At processblock 1110, a given component can be split from other components of thefirst mixed light. At process block 1120, the split given component canbe received by an optical sensor (160), and at process block 1130,responsive to the sensed physical or chemical quantity 1133, a sensedphase shift (e.g. 1055, 155) can be applied to the given component. Atprocess block 1140, the given component can be provided (e.g. tomodulator 150) for recombination. Then, at process block 1150, the givencomponent, incorporating a phase shift representative of a sensedquantity 1133, can be recombined with the other components.

First Example Detection Method

In a first example detection method, a response curve such as 510 or 520of FIG. 5 can be used directly to determine phase shift. By measuringpower and using a lookup table corresponding to a portion of responsecurve 510, the measured power can be directly transformed into anestimate of the sensed phase shift. Interpolation on the lookup tablecan be used. Optionally, a sensing system can be tuned such that abaseline point having a known value of a sensed quantity (or apredetermined value of sensed phase) corresponds to a target phase pointon response curve 510.

Second Example Detection Method

FIG. 12 is a flowchart 1200 illustrating a second example detectionmethod according to the disclosed technologies. The method is describedwith reference to the apparatus of FIG. 8 for convenience ofillustration, however the method is not limited to such apparatus. Atprocess block 1210, an auxiliary phase sweep can be applied to aselected light component to sweep a fringe pattern at a detector. Atprocess block 1220, a phase point of the phase sweep can be determinedwhich corresponds to a target point of the fringe pattern. At processblock 1230, a linear transformation can be applied to the determinedphase point to determine the sensed phase shift (e.g. 1055) that wasapplied to a given component prior to injection into the phase-sensitiveamplifier (e.g. 170). At process block 1240, the sensed phase shift canbe transformed into a measurement of the underlying sensed physical orchemical parameter. In examples, the target point of the fringe patterncan be a dark fringe point (e.g. 512).

Third Example Detection Method

FIG. 13 is a flowchart 1300 illustrating another example detectionmethod according to the disclosed technologies. The method is describedwith reference to the apparatus of FIG. 7 for convenience ofillustration, however the method is not limited to such apparatus. Atprocess block 1310, a compensatory phase shift can be applied to aselected light component based on feedback from an output of aphotosensor (e.g. 783), to obtain, at process block 1320, a targetfringe position at the photosensor (783). At process block 1330, alinear transformation can be applied to the compensatory phase shift todetermine the sensed phase shift (e.g. 1055) that was applied to a givencomponent prior to injection into the phase-sensitive amplifier (e.g.170). At process block 1340, the sensed phase shift can be transformedinto a measurement of the underlying sensed physical or chemicalparameter. In varying examples, the target fringe position can be a darkfringe point (e.g. 512) or a fringe position having steep response to achange of sensed phase (e.g. 514, 516).

Additional Method Variation Examples

Numerous further variations of the above methods are possible. Withreference to FIG. 10, seed probe light and pump light can be provided tothe first nonlinear lightguide by respective lasers. The seed probelight can be multiplexed between two or more wavelengths, andcorresponding sensed phase shifts can be incorporated into differentwavelength light components on a time-multiplexed basis. Thus, eachmultiplexed wavelength can be used to measure a respective physical orchemical property.

Example Optical Sensor

Turning back to FIG. 1, a combination of optical device 120 and detector180 can form an optical sensor. Detector 180 can be configured accordingto a technique described herein, or according to another technique, todetermine a representation of a sensed quantity from a sensed phaseshift (e.g. 155). Optionally, the optical sensor can be integrated witha sensor (e.g. 160) or probe and pump source lamps (e.g. 112, 114). APIC embodiment of an optical sensor can be a chip scale device.

In a first example, the phase sensing device of the optical sensor canbe coupled to a diaphragm or drum to sense a pressure wave. Such asensor can be used as a hydrophone or as an accelerometer.

In a second example, the phase sensing device can be a fiber coil,configured to develop a phase shift dependent on an angular velocity ofthe coil around the coil axis. In further examples, two fiber coilswound in opposite sense can be used for probe and conjugate componentsrespectively, to improve phase sensitivity. The two fiber coils can havematched length (and matched delay) and can be implemented with standardsingle-mode fiber. Such angular velocity sensors can be used asgyroscopes.

Example System

FIG. 14 is a block diagram of an optical sensing system 1400 accordingto the disclosed technologies. The sensing system 1400 incorporateslasers 1412, 1414 respectively providing seed probe light and pump lightto nonlinear lightguide 1430, which can be configured to generate mixedlight comprising probe, pump, and conjugate light components, forexample by a nonlinear mixing process. At least a given component of themixed light can be received by modulator 1450 and transported through anoptical sensor 1460 to incorporate a phase shift representative of asensed quantity. With phase shift incorporated, the given component canbe coupled to nonlinear lightguide 1470, which can be situated toreceive mixed light having probe, pump, and conjugate components. Theselight components include the given light component received from themodulator 1470, with sensed phase shift incorporated. Nonlinearlightguide 1470 can be configured to provide phase-sensitive gain toprobe and conjugate components. The system 1400 can be configured sothat the phase-sensitive gain, averaged over phase shift, can match theprobe gain of nonlinear lightguide 1430 (output probe power divided byinput seed probe power). Gain matching can be accomplished by selectionof lengths of lightguides 1430, 1470, by selection of pump power inlightguides 1430, 1470, by polarization shifting, or by any combinationof these or other techniques.

Sensing system 1400 further includes a photodetector 1480 coupled toreceive and detect at least one of probe or conjugate light componentsfrom lightguide 1470. Detector 1480 can also be coupled to a controlledphase shifter 1465 in the path of one of the light components betweenthe lightguides 1430, 1470. In varying examples, sensor 1460 and phaseshifter 1465 can be on the light path of a single component, or on lightpaths of different components. Controlled phase shifter 1465 can be usedfor a phase detection technique as described herein.

One or more of the blocks described can be connected to computer-basedmeasurement and control system 1490, which can include one or morecomputing environments, one or more controllers, and one or more dataacquisition subsystems. In addition to measurement and control duringnormal operation, measurement and control system 1490 can also be usedto tune or configure the sensing system 1400, for example to set pumppower level or seed frequency, to verify power levels, gains, or spectraat any points of the system, or to calibrate a detector.

In some examples, seed probe laser 1412 can be a CW laser. Pump laser1414 can be a pulsed laser. Numerous variations and configurations ofthe blocks of system 1400 are possible, as described for similar blocksof other examples herein.

Example Airborne System

FIG. 15 is a diagram 1500 of an airborne optical sensing systemaccording to the disclosed technologies. One or more interferometers1510 can be housed in an aircraft 1505 and coupled to one or moreoptical sensors 1561-1567 distributed around the aircraft 1505. Aninterferometer 1510 can incorporate nonlinear lightguides and otherblocks as describe in context of FIG. 14 or elsewhere herein. Fiberbundles 1541, 1544 can route light components among the optical sensors1561-1567, which can be fiber sensors.

The constituent fibers of bundles 1541, 1544 can be coupled to differentrespective interferometers 1510, or two or more fibers can share aninterferometer 1510, with multiplexing as described herein. The sensors1561-1567 can be on respective light paths of different components, ortwo or more sensors can be on a common light path and can be selectivelyenabled by an external control. Sensors 1561-1563 are illustrated asreflection mode sensors, while sensors 1564-1567 are illustrated astransmission mode sensors.

Sensors 1561-1567 can have intrinsic sensitivity to one or moreparameters and can provide a phase shift on a component of lighttransiting in and out of the sensor. The phase shift can vary inresponse to variations in a sensed parameter as described herein. Aninterferometer 1510 coupled to a sensor 1561-1567 can detect such aphase shift. With suitable sensors 1561-1567, the airborne opticalsensing system can provide indication of a wide variety of parametersassociated with aircraft 1505 including, without limitation: interior,skin, or exterior temperature; interior or exterior pressure; fuellevel; acoustic noise level; vibration; attitude (e.g. with a gyroscopicsensor); smoke; air pollution; engine or electrical parameters;condition monitoring; or airspeed.

Although aircraft 1505 is depicted as a fixed wing airplane, this is nota requirement. Similar systems can be deployed in a wide range ofairborne applications, including manned and unmanned aircraft (includinghelicopters, drones, balloons, satellites, or airships) used inpassenger, commercial, military, surveillance, remote sensing, ortelecommunication applications.

Example Downhole System

FIG. 16 is a diagram 1600 of a downhole optical sensing system accordingto the disclosed technologies. One or more interferometers 1610 can bedeployed proximate to a shaft 1605 and coupled to one or more sensors1661-1665 distributed along the shaft 1605. An interferometer 1610 canincorporate nonlinear lightguides and other blocks as describe incontext of FIG. 14 or elsewhere herein. Fiber bundles 1641, 1644 canroute light components among the optical sensors 1661-1665. Varyingconfigurations of fibers and sensors are possible, similar to thosedescribed in context of FIG. 15. As illustrated, sensors 1664-1665 canbe transmission mode sensors, while sensors 1661-1663 can be reflectionmode sensors. Couplers 1647-1648 can be used to tap light components atarbitrary positions along one or more fibers of bundle 1641. Measurementand control of instruments 1610 can be communicated over a wired,wireless, or optical network 1615 to or from a local or remote controlroom or monitoring station.

Similar to FIG. 15, each of sensors 1661-1665 can impose a sensed phaseshift on a transiting component of light, which can be measured by acoupled interferometer 1610. With suitable sensors 1661-1665, thedownhole optical sensing system can provide indication of a wide varietyof environmental parameters including, without limitation: temperature;air, gas, or liquid pressure; acoustic noise level; vibration; chemicalconcentration; or radioactivity.

The shaft 1605 can be an oil well, either production or exploratory, agas well, or a fluid injection or extraction shaft for fracking. Similarsystems can be deployed in other subterranean applications, for examplestorage tanks or access shafts in geologic formations. Further, similarsystems can be deployed over long pipelines for transport ofpetrochemicals or other fluids, or within a refinery or processingplant.

Second Example Device

A second example device is described with reference to FIG. 1. Asplitter 130 can be configured to split probe and conjugate modes(components) from a pump mode (component) within a nonlinear medium. Amodulator 150 can be coupled to receive one or more of the modes fromthe splitter at an input port (similar to port 451), and can further becoupled to provide the received modes to an output port (similar to port459). A given one of the provided modes can incorporate a phase shiftnot present in the corresponding received mode, the phase shiftrepresenting a sensed quantity. A mode coupling amplifier 170 can besituated to receive pump, probe, and conjugate modes, which collectivelycan include the given mode, with incorporated phase shift, coupled fromthe output port of the modulator. The pump and conjugate modes canundergo phase-sensitive gain in the mode coupling amplifier 170. Thesecond example device 120 can be used as an interferometer. Thephase-sensitive gain, averaged over values of the phase shift, can havea predetermined relationship with a probe gain experienced by the probemode in the splitter 130.

Numerous variations are possible within the scope of the disclosedtechnologies, as disclosed herein. For example, the nonlinear medium ofsplitter 130 can be a glass fiber with third order nonlinearsusceptibility. The splitting of modes can occur due to pump-degeneratefour-wave mixing. The splitter 130 and mode-coupling amplifier 170 canemploy a common gain mechanism. The incorporated phase shift in thegiven light mode can be provided by an external fiber sensor coupled tothe modulator in the light path of the given mode.

Example Experiment

Authors have fabricated an apparatus similar to that of FIG. 1, haveperformed measurements to confirm operation of the apparatus, aspredicted by computer simulations. Lightguides 130, 170 were constructedof identical HNLF fiber having lengths 131, 171 of 98 m and 510 mrespectively. The fiber was “ordinary dispersion” fiber, i.e. notdispersion-shifted, having a zero-dispersion wavelength of 1542 nm(corresponding to a frequency of 194.4 THz) and a nonlinearitycoefficient gamma of 9.3 W⁻¹km⁻¹.

A +12 dBm stabilized CW laser operating at 193.0 THz was used for seedprobe lamp 112. Pump lamp 114 was a mode-locked laser operating at194.05 THz, with pulses of approximately 5 ps flat-top duration at 33.3MHz, i.e. approximately 0.016% duty cycle, and about 40 dBm (10 W) peakinstantaneous power. Optocoupler 116 was implemented as an attenuatorand polarization controller (PC) on the pump laser output, apolarization controller on the seed laser output, followed by a 50-50coupler to mix seed and pump light, and a polarizer on the input tolightguide 130. The polarization controllers were used to align therespective lamp output polarizations with the linear polarization of thepolarizer. The pump attenuator was set to about the threshold for onsetof self-phase modulation (SPM).

Modulator 150 was implemented using a programmable optical pulse shaperhaving about 4.5 dB insertion loss. The lengths 131, 171 were chosen toprovide a match between probe gain of 15 dB and average phase-sensitivegain in lightguide 170, to counteract the insertion loss of modulator150, and for the light power levels described.

The output of lightguide 170 was sent through a bandpass filter anddetected with an avalanche photodiode for normal operation, and with abalanced photodiode pair for testing noise levels. Separately, opticalspectra were observed with an optical spectrum analyzer set to a 2 GHzresolution bandwidth.

In this experiment, a maximum fringe visibility of 97% wasexperimentally confirmed, with >90% visibility over a 554 GHz conjugatecomponent bandwidth. The bandwidth is sufficiently wide to supportsensing with multiple sensors in parallel, at respective wavelengths, asdescribed in context of FIG. 9. The noise characteristics and fringeshape were confirmed against simulations.

Further details have been provided in the authors' publication Lukens etal. “A broadband fiber-optic nonlinear interferometer,” vol. 113,article 091103 (2018), incorporated herein by reference.

A Generalized Computer Environment

FIG. 17 illustrates a generalized example of a suitable computing system1700 in which described examples, techniques, and technologies for anonlinear optical interferometer can be implemented. The computingsystem 1700 is not intended to suggest any limitation as to scope of useor functionality of the present disclosure, as the innovations can beimplemented in diverse general-purpose or special-purpose computingsystems. The computing system 1700 can control a disclosed opticalapparatus or optical sensing system; or can acquire, process, output, orstore measurement data.

With reference to FIG. 17, computing environment 1710 includes one ormore processing units 1722 and memory 1724. In FIG. 17, this basicconfiguration 1720 is included within a dashed line. Processing unit1722 can execute computer-executable instructions, such as for controlor data acquisition as described herein. Processing unit 1722 can be ageneral-purpose central processing unit (CPU), a processor in anapplication-specific integrated circuit (ASIC), or any other type ofprocessor. In a multi-processing system, multiple processing unitsexecute computer-executable instructions to increase processing power.Computing environment 1710 can also include a graphics processing unitor co-processing unit 1730. Tangible memory 1724 can be volatile memory(e.g., registers, cache, or RAM), non-volatile memory (e.g., ROM,EEPROM, or flash memory), or some combination thereof, accessible byprocessing units 1722, 1730. The memory 1724 stores software 1780implementing one or more innovations described herein, in the form ofcomputer-executable instructions suitable for execution by theprocessing unit(s) 1722, 1730. The memory 1724 can also store controlparameters, calibration data, measurement data, or database data. Thememory 1724 can also store configuration and operational data.

A computing system 1710 can have additional features, such as one ormore of storage 1740, input devices 1750, output devices 1760, orcommunication ports 1770. An interconnection mechanism (not shown) suchas a bus, controller, or network interconnects the components of thecomputing environment 1710. Typically, operating system software (notshown) provides an operating environment for other software executing inthe computing environment 1710, and coordinates activities of thecomponents of the computing environment 1710.

The tangible storage 1740 can be removable or non-removable, andincludes magnetic disks, magnetic tapes or cassettes, CD-ROMs, DVDs, orany other medium which can be used to store information in anon-transitory way and which can be accessed within the computingenvironment 1710. The storage 1740 stores instructions of the software1780 (including instructions and/or data) implementing one or moreinnovations described herein. Storage 1740 can also store image data,measurement data, configuration data, or other databases or datastructures described herein.

The input device(s) 1750 can be a mechanical, touch-sensing, orproximity-sensing input device such as a keyboard, mouse, pen,touchscreen, or trackball, a voice input device, a scanning device, oranother device that provides input to the computing environment 1710.The output device(s) 1760 can be a display, printer, speaker, opticaldisk writer, or another device that provides output from the computingenvironment 1710. Input or output can also be communicated to/from aremote device over a network connection, via communication port(s) 1770.

The communication port(s) 1770 enable communication over a communicationmedium to another computing entity. The communication medium conveysinformation such as computer-executable instructions, audio or videoinput or output, or other data in a modulated data signal. A modulateddata signal is a signal that has one or more of its characteristics setor changed in such a manner as to encode information in the signal. Byway of example, and not limitation, communication media can use anelectrical, optical, RF, acoustic, or other carrier.

In some examples, computer system 1700 can also include a computingcloud 1790 in which instructions implementing all or a portion of thedisclosed technology are executed. Any combination of memory 1724,storage 1740, and computing cloud 1790 can be used to store softwareinstructions and data of the disclosed technologies.

The present innovations can be described in the general context ofcomputer-executable instructions, such as those included in programmodules, being executed in a computing system on a target real orvirtual processor. Generally, program modules or components includeroutines, programs, libraries, objects, classes, components, datastructures, etc. that perform particular tasks or implement particulardata types. The functionality of the program modules can be combined orsplit between program modules as desired in various embodiments.Computer-executable instructions for program modules can be executedwithin a local or distributed computing system.

The terms “computing system,” “computing environment,” and “computingdevice” are used interchangeably herein. Unless the context clearlyindicates otherwise, neither term implies any limitation on a type ofcomputing system, computing environment, or computing device. Ingeneral, a computing system, computing environment, or computing devicecan be local or distributed, and can include any combination ofspecial-purpose hardware and/or general-purpose hardware and/orvirtualized hardware, together with software implementing thefunctionality described herein.

General Considerations

As used in this application, the singular forms “a,” “an,” and “the”include the plural forms unless the context clearly dictates otherwise.Additionally, the terms “includes” and “incorporates” mean “comprises.”Further, the term “coupled” encompasses mechanical, electrical,magnetic, optical, as well as other practical ways of coupling orlinking items together, and does not exclude the presence ofintermediate elements between the coupled items. Furthermore, as usedherein, the terms “or” and “and/or” mean any one item or combination ofitems in the phrase.

The systems, methods, and apparatus described herein should not beconstrued as being limiting in any way. Instead, this disclosure isdirected toward all novel and non-obvious features and aspects of thevarious disclosed embodiments, alone and in various combinations andsubcombinations with one another. The disclosed systems, methods, andapparatus are not limited to any specific aspect or feature orcombinations thereof, nor do the disclosed things and methods requirethat any one or more specific advantages be present or problems besolved. Furthermore, any features or aspects of the disclosedembodiments can be used in various combinations and subcombinations withone another.

Although the operations of some of the disclosed methods are describedin a particular, sequential order for convenient presentation, it shouldbe understood that this manner of description encompasses rearrangement,unless a particular ordering is required by specific language set forthbelow. For example, operations described sequentially can in some casesbe rearranged or performed concurrently. Moreover, for the sake ofsimplicity, the attached figures may not show the various ways in whichthe disclosed things and methods can be used in conjunction with otherthings and methods. Additionally, the description sometimes uses termslike “acquire,” “adjust,” “align,” “analyze,” “apply,” “calibrate,”“configure,” “detect,” “determine,” “display,” “estimate,” “form,”“generate,” “output,” “process,” “produce,” “read,” “store,”“transform,” “trigger,” “tune,” and “use” to describe operationsperformed or controlled by a computer in a computer system. These termsare high-level descriptions of the actual operations that are performedby a computer. The actual operations that correspond to these terms willvary depending on the particular implementation and are readilydiscernible by one of ordinary skill in the art.

Theories of operation, scientific principles, or other theoreticaldescriptions presented herein in reference to the apparatus or methodsof this disclosure have been provided for the purposes of betterunderstanding and are not intended to be limiting in scope. Theapparatus and methods in the appended claims are not limited to thoseapparatus and methods that function in the manner described by suchtheories of operation.

Any of the disclosed methods can be implemented as computer-executableinstructions or a computer program product stored on one or morecomputer-readable storage media, such as tangible, non-transitorycomputer-readable storage media, and executed on a computing device(e.g., any available computing device, including tablets, smart phones,or other mobile devices that include computing hardware). Tangiblecomputer-readable storage media are any available tangible media thatcan be accessed within a computing environment (e.g., one or moreoptical media discs such as DVD or CD, volatile memory components (suchas DRAM or SRAM), or nonvolatile memory components (such as flash memoryor hard drives)). By way of example, and with reference to FIG. 17,computer-readable storage media include memory 1724, and storage 1740.The term computer-readable storage media does not include signals andcarrier waves. In addition, the term computer-readable storage mediadoes not include communication ports (e.g., 1770).

Any of the computer-executable instructions for implementing thedisclosed techniques as well as any data created and used duringimplementation of the disclosed embodiments can be stored on one or morecomputer-readable storage media. The computer-executable instructionscan be part of, for example, a dedicated software application or asoftware application that is accessed or downloaded via a web browser orother software application (such as a remote computing application).Such software can be executed, for example, on a single local computer(e.g., any suitable commercially available computer) or in a networkenvironment (e.g., via the Internet, a wide-area network, a local-areanetwork, a client-server network, a cloud computing network, or othersuch network) using one or more network computers.

For clarity, only certain selected aspects of the software-basedimplementations are described. Other details that are well known in theart are omitted. For example, it should be understood that the disclosedtechnology is not limited to any specific computer language or program.For instance, the disclosed technology can be implemented by softwarewritten in ABAP, Adobe Flash, C, C++, C#, Curl, Dart, Fortran, Java,JavaScript, Julia, Lisp, Matlab, Octave, Perl, Python, Qt, R, Ruby, SAS,SPSS, SQL, WebAssembly, any derivatives thereof, or any other suitableprogramming language, or, in some examples, markup languages such asHTML or XML, or with any combination of suitable languages, libraries,and packages. Likewise, the disclosed technology is not limited to anyparticular computer or type of hardware. Certain details of suitablecomputers and hardware are well known and need not be set forth indetail in this disclosure.

Furthermore, any of the software-based embodiments (comprising, forexample, computer-executable instructions for causing a computer toperform any of the disclosed methods) can be uploaded, downloaded, orremotely accessed through a suitable communication means. Such suitablecommunication means include, for example, the Internet, the World WideWeb, an intranet, software applications, cable (including fiber opticcable), magnetic communications, electromagnetic communications(including RF, microwave, infrared, and optical communications),electronic communications, or other such communication means.

The disclosed methods, apparatus, and systems should not be construed aslimiting in any way. Instead, the present disclosure is directed towardall novel and nonobvious features and aspects of the various disclosedembodiments, alone and in various combinations and subcombinations withone another. The disclosed methods, apparatus, and systems are notlimited to any specific aspect or feature or combination thereof, nor dothe disclosed embodiments require that any one or more specificadvantages be present or problems be solved. The technologies from anyexample can be combined with the technologies described in any one ormore of the other examples.

In view of the many possible embodiments to which the principles of thedisclosed subject matter may be applied, it should be recognized thatthe illustrated embodiments are only preferred examples of the disclosedsubject matter and should not be taken as limiting the scope of theclaims. Rather, the scope of the claimed subject matter is defined bythe following claims. We therefore claim as our invention all that comeswithin the scope of these claims and their equivalents.

We claim:
 1. An optical device, comprising: a first nonlinear lightguidehaving a first length and being situated to receive seed probe light andpump light from respective light sources and being configured to formfirst mixed light comprising first probe, first pump, and firstconjugate light components, the seed probe light undergoing a probe gainin the first nonlinear lightguide; a modulator situated to receive thefirst mixed light from the first nonlinear lightguide and output secondmixed light comprising second probe, second pump, and second conjugatelight components, wherein a given component among the second probe,second pump, and second conjugate light components incorporates anon-zero phase shift, representative of a sensed quantity, relative to acorresponding component among the first probe, first pump and firstconjugate light components; and a second nonlinear lightguide having asecond length, situated to receive the second mixed light from themodulator and apply phase-sensitive amplification on the second probeand second conjugate light components; wherein the second length islarger than the first length such that averaged phase-sensitiveamplification applied by the second nonlinear lightguide matches theprobe gain in the first nonlinear lightguide.
 2. The optical device ofclaim 1, further comprising: a photodetector coupled to an output of thesecond nonlinear lightguide and configured to measure at least one ofthe second probe light component or the second conjugate light componentto determine the phase shift.
 3. The optical device of claim 2, furthercomprising: a controlled phase shifter coupled to the photodetector andsituated in a path of one of the components of the first mixed lightbetween the first and second nonlinear lightguides.
 4. An opticalsensing system comprising: the optical device of claim 3; a first laseras the light source from which the seed probe light is received; and asecond laser as the light source from which the pump light is received.5. An airborne monitoring system comprising: the optical sensing systemof claim 4 situated on an aircraft, wherein the sensed quantity is aparameter of the aircraft to be monitored; and a fiber sensor coupled tothe modulator, wherein the fiber sensor has intrinsic sensitivity to theparameter and provides the phase shift in the given component, whereinthe phase shift varies responsive to variations in the parameter.
 6. Adown-hole environmental monitoring system comprising: the opticalsensing system of claim 4 situated proximate to a petrochemical accessshaft, wherein the sensed quantity is an environmental parameter to bemonitored within the petrochemical access shaft; and a fiber sensorcoupled to the modulator, wherein the fiber sensor has intrinsicsensitivity to the environmental parameter and provides the phase shiftin the given component, wherein the phase shift varies responsive tovariations in the environmental parameter.
 7. An optical sensorcomprising: the optical device of claim 2; and a circuit coupled to anoutput of the photodetector and configured to transform the determinedphase shift into a representation of the sensed quantity.
 8. The opticalsensor of claim 7, wherein the sensed quantity is a pressure wave andthe optical sensor is a hydrophone.
 9. The optical sensor of claim 7,wherein the sensed quantity is an angular velocity and the opticalsensor is a gyroscope.
 10. The optical device of claim 1, wherein: thesensed quantity is one or more of: temperature, strain, pressure, orangular velocity; and the phase shift is incorporated into the givencomponent by an intrinsic fiber sensor that is sensitive to the sensedquantity.
 11. The optical device of claim 1, wherein at least one of thefirst or second nonlinear lightguides is an optical fiber.
 12. Theoptical device of claim 1, wherein at least one of the first or secondnonlinear lightguides is a waveguide in a planar lightwave circuit. 13.The optical device of claim 1, wherein the first and second nonlinearlightguides have matching cross-sectional structure and matchingcomposition.
 14. The optical device of claim 1, wherein the probe gainis obtained by pump-degenerate four-wave mixing.
 15. The optical deviceof claim 1, wherein the modulator comprises: a splitter configured toseparate the corresponding component from other components of the firstmixed light; and a recombiner configured to merge the given component,with the phase shift incorporated, with other components of the secondmixed light.
 16. The optical device of claim 15, wherein the splitterand the recombiner are implemented as an optical add-drop multiplexer(OADM).
 17. The optical device of claim 15, further comprising: a fibersensor situated to transport the corresponding component from thesplitter, develop the phase shift, and transport the given component,with the phase shift incorporated, to the recombiner.
 18. The opticaldevice of claim 15, wherein the modulator further comprises: a firstport for coupling the corresponding component from the splitter to anexternal fiber sensor; and a second port for coupling the givencomponent, with the phase shift incorporated, from the external fibersensor to the recombiner.
 19. The optical device of claim 1, wherein:the seed probe light is multiplexed between a plurality of wavelengths;the corresponding component of the first mixed light is correspondinglymultiplexed between respective sensors for the plurality of wavelengths;and the sensed quantity is correspondingly multiplexed between arespective plurality of quantities detected by the respective sensors.20. The optical device of claim 1, wherein the given component is thesecond probe light component, the corresponding component is the firstprobe light component; and wherein the second pump and second conjugatelight components have phase relationships with the first pump and firstconjugate light components, respectively, that are independent of thephase shift representative of the sensed quantity.
 21. The opticaldevice of claim 1, wherein the given component is the second conjugatelight component, the corresponding component is the first conjugatelight component; and wherein the second pump and second probe lightcomponents have phase relationships with the first pump and first probelight components, respectively, that are independent of the phase shiftrepresentative of the sensed quantity.
 22. The optical device of claim1, wherein the given component is the second pump light component, thecorresponding component is the first pump light component; and whereinthe second probe and second conjugate light components have phaserelationships with the first probe and first conjugate light components,respectively, that are independent of the phase shift representative ofthe sensed quantity.
 23. The optical device of claim 1, wherein afurther component of the second mixed light, excluding the givencomponent, and a further component of the first mixed light, excludingthe corresponding component, have a phase relationship that is dependenton the phase shift representative of the sensed quantity.
 24. Theoptical device of claim 1, wherein the sensed quantity is anenvironmental parameter.
 25. The optical device of claim 1, wherein thelight sources are lasers.